Item Name | Panel Structural Aircraft |
Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
Federal Supply Class (FSC) | 1560 Airframe Structural Components |
National Item Identification Number (NIIN) | 01-370-9808 (013709808) |
NCB Code | USA (01) |
Manufacturer | Boeing Company The |
Part Number | Manufacturer | Item Name | Cage Code | RFQ |
---|---|---|---|---|
17P2A6022-5 | boeing company the | panel structural aircraft | 88277 | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | LAMINATED AND COMPOSITE |
SR-5 | MANUFACTURERS CODE | 88277 |
CZEJ | AIRCRAFT STATION NUMBER | FS 981.500 TO FS 1045.75 |
SR-5 | DESIGN CONTROL REFERENCE | 17P2A6022-5 |
CZDJ | AIRCRAFT LOCATION | CENTER FUSELAGE,WING FILLET,CLOSEOUT |
BWJF | SIDE FOR WHICH DESIGNED | LEFT SIDE |
SFTT | SURFACE TREATMENT | PRIMER EPOXY |
CZEK | AIRCRAFT MISSION DESIGN SERIES | C-17A |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | DMS1974 MFR REF 1ST MATERIAL RESPONSE AND DMS2288 MFR REF 2ND MATERIAL RESPONSE |
SR-5 | THE MANUFACTURERS DATA | |
FEAT | SPECIAL FEATURES | NHA 17P2A6022-3;PANEL INSTL,FILLET CLOSEOUT-Y=981.50 TO Y=1045.75 |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE |
MATT | MATERIAL | PLASTIC POLYAMIDE AND PLASTIC ARAMID |
Relevant Components for NSN - 1560-01-370-9808, 1560013709808 | ||||
1560-01-141-9838 (1560011419838) | 1560-00-588-2363 (1560005882363) | 1560-01-252-8219 (1560012528219) | 1560-01-388-6401 (1560013886401) | |
1560-01-008-7294 (1560010087294) | 1560-00-366-9982 (1560003669982) | 1560-00-536-7361 (1560005367361) | 1560-01-027-6767 (1560010276767) | |
1560-01-287-5477 (1560012875477) | 1560-01-605-0677 (1560016050677) | 1560-01-237-9622 (1560012379622) | 1560-01-533-6724 (1560015336724) | |
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